Far 23 pdf

(1) The airplane is assumed to be subjected to symmetrical vertical gusts in level flight. The resulting limit load factors must correspond to the conditions determined as follows: (i) Positive (up) and negative (down) gusts of 50 f.p.s. at V C must be considered at altitudes between sea level and 20,000 feet. Sec. 23.221 Spinning. [(a) Normal category airplanes.A single-engine, normal category airplane must be able to recover from a one-turn spin or a three-second spin, whichever takes longer, in not more than one additional turn after initiation of the first control action for recovery, or demonstrate compliance with the optional spin resistant requirements of this section. Home | Acquisition.GOV AND ASSESSMENT FOR PART 23 AIRPLANES Date: 1/16/09 Initiated by: ACE-100 AC No: 23.1309-1D This advisory circular (AC) sets forth an acceptable means of showing compliance with Title 14 of the Code of Federal Regulations (14 CFR) § 23.1309(a) and (b) (Amendment 23-49) for equipment, systems, and installations in 14 CFR part 23 airplanes. § 23.1457 Cockpit voice recorders. § 23.1459 Flight data recorders. § 23.1529 Instructions for continued airworthiness. Subpart A - General (§§ 23.2000 - 23.2010) Subpart B - Flight (§§ 23.2100 - 23.2165) Subpart C - Structures (§§ 23.2200 - 23.2270) Subpart D - Design and Construction (§§ 23.2300 - 23.2335) Part 23 - AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND COMMUTER CATEGORY AIRPLANES Date January 1, 2011 Authority 49 U.S.C. 106 (g), 40113, 44701-44702, 44704. Source Docket No. 4080, 29 FR 17955, Dec. 18. 1964; 30 FR 258, Jan. 9, 1965, unless otherwise noted. Federal Register References 29 FR 17955, 30 FR 258 Under current 14 CFR Part 23, airplanes are certified in one or more of the following categories: normal, utility, acrobatic, and commuter. Classification primarily depends upon the types of maneuvers to be performed, number of seats, number of engines, and maximum certificated takeoff weight. 13. Will the FAA continue to certify airplanes in 25.23 Load distribution limits. 25.25 Weight limits. 25.27 Center of gravity limits. 25.29 Empty weight and corresponding center of gravity. 25.31 Removable ballast. 25.33 Propeller speed and pitch limits. PERFORMANCE 25.101 General. 25.103 Stall speed. 25.105 Takeoff. 25.107 Takeoff speeds. 25.109 Accelerate-stop distance. 25.111 Takeoff path. Para # 23 (pdf) Author: alkalam.pk Subject: Al-Qur'an Indo-Pak Style Created Date: 5/18/2004 12:48:30 PM eCFR Content § 23.2005 Certification of normal category airplanes. ( a) Certification in the normal category applies to airplanes with a passenger-seating configuration of 19 or less and a maximum certificated takeoff weight of 19,000 pounds or less. ( b) Airplane certification levels are: • In 2017, the FAA implemented amendment 23-64 to part 23 airworthiness standards for normal category airplanes • This briefing will address: 1. Reasons for change 2. Characteristics of performance- based rules 3. Key aspects of amendment 23- 64 4. Means of compliance to part 23 5. Consensus standards and ASTM International 6. Additional 23 Subpart K-Approval of Materials, Parts, Processes, and Appliances 191 24 Subpart L-Export Airworthiness Approvals 195 25 Subpart M-Designated Alteration Station Authorization Procedures 203 26 Subpart N-Approval of Engines, Propellers, Materials, Parts, and Ap-pliances : Import 209 27 Subpart O-Technical Standard Order 23 Subpart K-Approval of Materials, Parts, Processes, and Appliances 191 24 Subpart L-Export Airworthi